ATE550520T1 - Vibrationsdämpfer für turbomaschinenschaufelaufsätze, zugehörige turbomaschine und zugehörige motoren - Google Patents

Vibrationsdämpfer für turbomaschinenschaufelaufsätze, zugehörige turbomaschine und zugehörige motoren

Info

Publication number
ATE550520T1
ATE550520T1 AT09804573T AT09804573T ATE550520T1 AT E550520 T1 ATE550520 T1 AT E550520T1 AT 09804573 T AT09804573 T AT 09804573T AT 09804573 T AT09804573 T AT 09804573T AT E550520 T1 ATE550520 T1 AT E550520T1
Authority
AT
Austria
Prior art keywords
turbo machine
vibration dampers
blades
motors
pocket
Prior art date
Application number
AT09804573T
Other languages
German (de)
English (en)
Inventor
Adrien Fabre
Original Assignee
Snecma
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Snecma filed Critical Snecma
Application granted granted Critical
Publication of ATE550520T1 publication Critical patent/ATE550520T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/70—Treatment or modification of materials
    • F05D2300/702—Reinforcement
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Harvester Elements (AREA)
AT09804573T 2008-08-06 2009-08-05 Vibrationsdämpfer für turbomaschinenschaufelaufsätze, zugehörige turbomaschine und zugehörige motoren ATE550520T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0855448A FR2934873B1 (fr) 2008-08-06 2008-08-06 Dispositif amortisseur de vibrations pour attaches d'aubes.
PCT/EP2009/060165 WO2010015660A1 (fr) 2008-08-06 2009-08-05 Dispositif amortisseur de vibrations pour attaches d'aubes de turbomachine, turbomachine et moteurs associes

Publications (1)

Publication Number Publication Date
ATE550520T1 true ATE550520T1 (de) 2012-04-15

Family

ID=40427286

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09804573T ATE550520T1 (de) 2008-08-06 2009-08-05 Vibrationsdämpfer für turbomaschinenschaufelaufsätze, zugehörige turbomaschine und zugehörige motoren

Country Status (11)

Country Link
US (1) US8801385B2 (pt)
EP (1) EP2324205B1 (pt)
JP (1) JP5430657B2 (pt)
CN (1) CN102112702B (pt)
AT (1) ATE550520T1 (pt)
BR (1) BRPI0917586B1 (pt)
CA (1) CA2732032C (pt)
ES (1) ES2382985T3 (pt)
FR (1) FR2934873B1 (pt)
RU (1) RU2503825C2 (pt)
WO (1) WO2010015660A1 (pt)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201106278D0 (en) * 2011-04-14 2011-05-25 Rolls Royce Plc Annulus filler system
US9410439B2 (en) 2012-09-14 2016-08-09 United Technologies Corporation CMC blade attachment shim relief
CN103808515B (zh) * 2012-11-12 2016-08-03 中航商用航空发动机有限责任公司 叶片分离装置以及发动机包容性试验装置
JP6150548B2 (ja) * 2013-02-13 2017-06-21 三菱重工業株式会社 回転機械翼
JP6151932B2 (ja) * 2013-02-28 2017-06-21 三菱重工業株式会社 回転機械用減衰部材
US10519788B2 (en) 2013-05-29 2019-12-31 General Electric Company Composite airfoil metal patch
CN104500447A (zh) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 风洞轴流压缩机风扇
CN104500446A (zh) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 风洞轴流压缩机转子复合材料叶片根部连接结构
KR101607780B1 (ko) * 2014-12-24 2016-03-30 두산중공업 주식회사 도브테일의 고정장치 및 이의 고정방법
EP3307989B1 (de) * 2015-08-19 2020-09-30 Siemens Aktiengesellschaft Gasturbinenschaufel oder verdichterschaufel mit anti-fretting-beschichtung im schaufelfussbereich und rotor
US10099323B2 (en) * 2015-10-19 2018-10-16 Rolls-Royce Corporation Rotating structure and a method of producing the rotating structure
FR3052485B1 (fr) * 2016-06-08 2019-05-10 Safran Aircraft Engines Rotor a element de dissipation d'energie
US20190112935A1 (en) * 2017-10-16 2019-04-18 United Technologies Corporation Gap closing wearliner
FR3078096B1 (fr) * 2018-02-20 2020-03-06 Arianegroup Sas Rotor pour turbomachine et turbomachine comprenant ce rotor
US11021972B2 (en) * 2018-08-14 2021-06-01 Rolls-Royce North American Technologies Inc. Variable pitch blade holder for gas turbine engine
FR3099213B1 (fr) * 2019-07-23 2021-07-16 Safran Aircraft Engines Rotor de soufflante pour une turbomachine d’aeronef
CN111022126A (zh) * 2019-11-19 2020-04-17 中国航发沈阳黎明航空发动机有限责任公司 一种转子密封减振结构
FR3107724B1 (fr) 2020-02-27 2022-06-24 Safran Aircraft Engines Rotor de soufflante à aubes à calage variable et turbomachine équipée d’un tel rotor
DE102020122318A1 (de) * 2020-08-26 2022-03-03 Ebm-Papst Mulfingen Gmbh & Co. Kg Lüfterradsystem zur Zusammenstellung und Herstellung eines Lüfterrades
CN112412541B (zh) * 2020-11-05 2022-07-15 中国航发沈阳发动机研究所 一种带凸肩一级转子结构
FR3126446B1 (fr) * 2021-09-01 2024-07-12 Safran Aircraft Engines Amortisseur déformable pour roue mobile de turbomachine
JP2023093088A (ja) 2021-12-22 2023-07-04 三菱重工業株式会社 回転機械

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1025421B (de) * 1955-10-31 1958-03-06 Maschf Augsburg Nuernberg Ag Befestigung von Lauftschaufeln sproeden Werkstoffes in metallischem Schaufeltraeger
US3842945A (en) * 1971-05-13 1974-10-22 J Potter Viscoelastic damper
SU418618A1 (pt) * 1972-01-25 1974-03-05
SU435360A1 (ru) * 1972-06-13 1974-07-05 В. Э. Гохберг, В. Д. Шалаев , В. Н. Шеповалов Устройство для демпфирования колебаний рабочих лопаток турбомашины
DE3815977A1 (de) * 1988-05-10 1989-11-30 Mtu Muenchen Gmbh Folienzwischenlage zur fuegung von reibkorrosionsgefaehrdeten maschinenbauteilen
JP2718131B2 (ja) * 1989-01-23 1998-02-25 石川島播磨重工業株式会社 ガスタービンディスク
RU2022120C1 (ru) * 1991-06-05 1994-10-30 Самарский государственный аэрокосмический университет им.акад.С.П.Королева Рабочее колесо осевой турбомашины
US5240375A (en) * 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade
US6102664A (en) * 1995-12-14 2000-08-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Blading system and method for controlling structural vibrations
US6132175A (en) * 1997-05-29 2000-10-17 Alliedsignal, Inc. Compliant sleeve for ceramic turbine blades
US6431835B1 (en) * 2000-10-17 2002-08-13 Honeywell International, Inc. Fan blade compliant shim
FR2841933B1 (fr) * 2002-07-04 2004-12-03 Snecma Moteurs Cale autobloquante
JP4352757B2 (ja) * 2003-05-14 2009-10-28 株式会社Ｉｈｉ ジェットエンジン用ファン及びファンスペーサ
RU2264561C1 (ru) * 2004-06-08 2005-11-20 Аверичкин Павел Алексеевич Ступень осевого компрессора газотурбинного двигателя
FR2890684B1 (fr) * 2005-09-15 2007-12-07 Snecma Clinquant pour aube de turboreacteur
FR2918702B1 (fr) * 2007-07-13 2009-10-16 Snecma Sa Clinquant pour aube de turbomachine

Also Published As

Publication number Publication date
EP2324205A1 (fr) 2011-05-25
FR2934873A1 (fr) 2010-02-12
RU2011108552A (ru) 2012-09-20
CN102112702A (zh) 2011-06-29
FR2934873B1 (fr) 2011-07-08
BRPI0917586B1 (pt) 2020-02-04
CA2732032C (fr) 2017-05-30
JP5430657B2 (ja) 2014-03-05
RU2503825C2 (ru) 2014-01-10
CA2732032A1 (fr) 2010-02-11
BRPI0917586A2 (pt) 2015-11-17
ES2382985T3 (es) 2012-06-15
US20110206530A1 (en) 2011-08-25
US8801385B2 (en) 2014-08-12
JP2011530038A (ja) 2011-12-15
CN102112702B (zh) 2014-03-12
EP2324205B1 (fr) 2012-03-21
WO2010015660A1 (fr) 2010-02-11

Similar Documents

Publication Publication Date Title
ATE550520T1 (de) Vibrationsdämpfer für turbomaschinenschaufelaufsätze, zugehörige turbomaschine und zugehörige motoren
WO2014197119A3 (en) Rotors with modulus mistuned airfoils
GB2459366B (en) A fan rotor for a turbomachine or a test engine
EP2500520A3 (en) Damper and seal pin arrangement for a turbine blade
WO2013165515A3 (en) Gas turbine engine with fan-tied inducer section
DE602006002673D1 (de) Vibrationsdämpfungselemente für einen axialen Haltering von Bläserschaufeln einer Turbomaschine
EP3640434A3 (en) Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine
DE602006006387D1 (de) Halterung und Verfahren für das Schleifen von Endteile der Turbinen-Rotorschaufeln
EP2239422A3 (en) Seal for a gas turbine engine
ATE547591T1 (de) Leitschaufel für eine axial durchströmbare turbomaschine und zugehörige leitschaufelanordnung
FR2926604B1 (fr) Centrage d'une piece a l'interieur d'un arbre de rotor dans une turbomachine
ATE538287T1 (de) Läufer einer gasturbine
MX2009012521A (es) Arreglo de alabes de rotor, especialmente para una turbina de gas.
EP2738392A3 (en) Fan blade for a turbofan gas turbine engine
ATE513736T1 (de) Hubschrauberrotor
DE602008002103D1 (de) Axiale Haltevorrichtung für Laufradschaufeln, die auf einer Rotorscheibe einer Strömungsmaschine montiert sind
DE602008005216D1 (de) Gasturbinenmotor mit Antriebsmittel für das Zubehörgehäuse und Montageverfahren für besagten Motor
FR2971816B1 (fr) Arbre d'entrainement de boitier a engrenages de machines auxiliaires d'un turboreacteur
BR112015005209A2 (pt) lâmina de ventilador para um motor de turbina a gás e conjunto de rotor.
EP2781694A3 (en) A composite vane
FR2934246B1 (fr) Aeronef comprenant au moins un moteur a rotors contrarotatifs
EP2481887A3 (en) Intershaft seal with support linkage
GB201110008D0 (en) Rotor casing structure
DE602008003880D1 (de) Turbinenstator für Turbotriebwerk eines Luftfahrzeugs, der mit einer Schwingungsdämpfungsvorrichtung ausgestattet ist
BR112014026221A2 (pt) turbocarregador de exaustão com mancal de bucha flutuante